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Flow Straightener for a Rotating-Drum Liquid SeparatorA flow straightener has been incorporated into a rotary liquid separator that originally comprised an inlet tube, a shroud plate, an impeller, an inner drum, an outer drum, a housing, a pitot tube, and a hollow shaft motor. As a consequence of the original geometry of the impeller, shroud, inner drum, and hollow shaft, swirl was created in the airflow inside the hollow shaft during operation. The swirl speed was large enough to cause a significant pressure drop. The flow straightener consists of vanes on the back side of the shroud plate. These vanes compartmentalize the inside of the inner drum in such a way as to break up the flow path and thereby stop the air from swirling; as a result, the air enters the hollow shaft with a predominantly axial velocity instead of a swirl. Tests of the rotary liquid separator at an airflow rate of 10 cu ft/min (0.0047 cu m/s) revealed that the dynamic pressure drop was 8 in. of water (approx.=2 kPa) in the absence of the flow straightener and was reduced to 1 in. of water (approx.=0.25 kPa) in the presence of the flow straightener.
Document ID
20110016781
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
O'Coin, James R.
(Hamilton Sundstrand Space Systems International, Inc. United States)
Converse, David G.
(Hamilton Sundstrand Space Systems International, Inc. United States)
Rethke, Donald W.
(Hamilton Sundstrand Space Systems International, Inc. United States)
Date Acquired
August 25, 2013
Publication Date
April 1, 2004
Publication Information
Publication: NASA Tech Briefs, April 2004
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MSC-23149
Report Number: MSC-23149
Distribution Limits
Public
Copyright
Public Use Permitted.
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